Home
Class 12
MATHS
A air-foce plane is ascending vertically...

A air-foce plane is ascending vertically at the rate of 100 km/h. If the radius of the earth is r km, how fast is the area of the earth, visible from the plane, increasing at 3 min after it started ascending?
Note Visible area `A=(2pir^(2)h)/(r+h)`, where h is the height of the plane above the earth.

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem step by step, we will follow these instructions: ### Step 1: Understand the Formula for Visible Area The visible area \( A \) of the Earth from the plane is given by the formula: \[ A = \frac{2 \pi r^2 h}{r + h} \] where \( r \) is the radius of the Earth and \( h \) is the height of the plane above the Earth's surface. ### Step 2: Differentiate the Area with Respect to Time We need to find how fast the area \( A \) is increasing, which means we need to differentiate \( A \) with respect to time \( t \): \[ \frac{dA}{dt} = \frac{d}{dt} \left( \frac{2 \pi r^2 h}{r + h} \right) \] Using the quotient rule, we differentiate: \[ \frac{dA}{dt} = 2 \pi r^2 \cdot \frac{(r + h) \frac{dh}{dt} - h \frac{d}{dt}(r + h)}{(r + h)^2} \] Since \( r \) is constant (the radius of the Earth), \( \frac{dr}{dt} = 0 \). ### Step 3: Simplify the Derivative Substituting \( \frac{dr}{dt} = 0 \) into the equation gives: \[ \frac{dA}{dt} = \frac{2 \pi r^2 \left( (r + h) \frac{dh}{dt} - h \cdot 0 \right)}{(r + h)^2} \] This simplifies to: \[ \frac{dA}{dt} = \frac{2 \pi r^2 (r + h) \frac{dh}{dt}}{(r + h)^2} \] ### Step 4: Calculate Height \( h \) After 3 Minutes The plane ascends at a rate of \( 100 \) km/h. After \( 3 \) minutes, we convert minutes to hours: \[ 3 \text{ minutes} = \frac{3}{60} \text{ hours} = \frac{1}{20} \text{ hours} \] Now, calculate \( h \): \[ h = \text{speed} \times \text{time} = 100 \text{ km/h} \times \frac{1}{20} \text{ h} = 5 \text{ km} \] ### Step 5: Substitute Values into the Derivative Now we substitute \( h = 5 \) km and \( \frac{dh}{dt} = 100 \) km/h into the derivative: \[ \frac{dA}{dt} = \frac{2 \pi r^2 (r + 5) \cdot 100}{(r + 5)^2} \] This simplifies to: \[ \frac{dA}{dt} = \frac{200 \pi r^2}{r + 5} \] ### Final Step: Conclusion Thus, the rate at which the area of the Earth visible from the plane is increasing at 3 minutes after it started ascending is: \[ \frac{dA}{dt} = \frac{200 \pi r^2}{r + 5} \text{ km}^2/\text{h} \]
Promotional Banner

Topper's Solved these Questions

  • DY / DX AS A RATE MEASURER AND TANGENTS, NORMALS

    ARIHANT MATHS|Exercise Exercise For Session 2|6 Videos
  • DY / DX AS A RATE MEASURER AND TANGENTS, NORMALS

    ARIHANT MATHS|Exercise Exercise For Session 3|10 Videos
  • DY / DX AS A RATE MEASURER AND TANGENTS, NORMALS

    ARIHANT MATHS|Exercise Exercise (Questions Asked In Previous 13 Years Exam)|7 Videos
  • DIFFERENTIATION

    ARIHANT MATHS|Exercise Exercise For Session 10|4 Videos
  • ELLIPSE

    ARIHANT MATHS|Exercise Exercise (Questions Asked In Previous 13 Years Exam)|27 Videos

Similar Questions

Explore conceptually related problems

An airforce plane is ascending vertically at the rate of 100km/h .If the radius of the earth is rkm, how fast is the area of the earth,visible from the plane,increasing at 3 minutes after it started ascending? Given that the visible area A at height h is given by A=2 pi r^(2)(h)/(r+h) .

A geostationary satellite is at a height h above the surface of earth. If earth radius is R -

A body of mass m is kept at a small height h above the ground. If the radius of the earth is R and its mass is M, the potential energy of the body and earth system (with h=infty being the reference position) is

At what height h above the earth's surface, the value of g becomes g/2 (where R is the radius of the earth)

A geostationary satellite is nearly at a height of h = 6 R from the surface of the earth where R is the radius of the earth. Calculate the area on the surface of the earth in which the communication can be made using this satellite.

The value of gravitational accelerationg at a height h above the earth's surface is then (R = radius of earth)

A cosmonaut is orbiting the earth in a spacecraft at an altitude h =630km with a speed of 8kms^(-2) . If the radius of the earth is 6400km, the acceleration of the cosmonaut is